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Flight Instructors Training Procedures _revised AIC_x

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IMPORTANT:<br />

ENTRY CHARACTERISTICS RECOVERY<br />

This lesson is based on a<br />

deliberately induced erect spin to<br />

the left. (Piper Cherokee 140)<br />

SAFETY:<br />

Calculate weight and Balance<br />

for utility category manoeuvre.<br />

Carry out HASELL checks<br />

Line up overhead a distinct<br />

line feature e.g. coastline.<br />

Height is calculated according to the<br />

specific aircraft type spin<br />

characteristics.<br />

E.g. PA28.140 looses 500’ for each<br />

rotation of spin.<br />

(A spitfire fighter loses 5000’ for each<br />

rotation .<br />

A fighter jet can lose up to 20 000’<br />

before recovery)<br />

CONTROL INPUTS:<br />

• Reduce speed in level flight, power<br />

off, clean configuration to ± 75 MPH<br />

• Simultaneously and abruptly apply<br />

FULL LEFT RUDDER and FULL<br />

UP ELEVATOR and hold the<br />

controls FULLY against the stops.<br />

• The aircraft will pitch nose up<br />

(STALL) and yaw (LEFT WING<br />

WILL STALL AND DROP) causing<br />

autorotation. HOLD THE<br />

CONTROLS FULLY DEFLECTED.<br />

BASED ON CHEROKEE 140<br />

TWO ROTATION SPIN<br />

• Steep nose-up pitch initially followed<br />

by wing drop to the left.<br />

• Low airspeed.<br />

• Nose rapidly pitches down yawing<br />

towards the left wing as autorotation<br />

starts.<br />

• The first rotation accelerates as the<br />

first 360° change of direction is<br />

completed.<br />

• The second rotation is considerably<br />

faster with a near vertical nose down<br />

attitude.<br />

• The airspeed is relatively low.<br />

*)<br />

Since the aircraft is stalled and yawed<br />

(Autorotation) we need to stop the yaw<br />

and unstall the aircraft.<br />

The following is based on the standard<br />

recovery procedure placarded in the<br />

Cherokee 140.<br />

• Confirm power off.<br />

• Ailerons neutral.<br />

• Apply FULL OPPOSITE RUDDER to<br />

the direction of rotation and ...<br />

• Apply positive forward movement of<br />

the control column TO THE CENTRE<br />

POSITION.<br />

Do not apply control column fully<br />

forwards as this will induce inverted<br />

flight!<br />

• As rotation stops centralise rudders<br />

and simultaneously ease the A/C out<br />

of the dive.<br />

• As the nose cuts the horizon check the<br />

airspeed is below 100mph and apply<br />

full power.<br />

• Climb back to entry altitude and carry<br />

out after take-off and HELL checks.<br />

Note: The height loss<br />

!"#$ # &"" '$ #

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